PA-28-181
INSPECTION REPORT
ARCHER II
ARCHER III
PIPER AIRCRAFT CORPORATION
(PART NUMBER 230 1039)
REISSUED: JULY 30, 1994
THIS PAGE INTENTIONALLY LEFT BLANK
PIPER AIRCRAFT CORPORATION
INSPECTION REPORT
7.
8.
9.
15. Inspect cylinders for cracked or broken fins.
(See Note 9.) ........................................................
16. Inspect rocker box covers for evidence of oil
leaks. If found, replace gasket; tighten cover
screws to a torque of 50 inch-pounds. (See Note
10.) .......................................................................
17. Inspect ignition harness and insulators for high
tension leakage and continuity. ............................
18. Inspect magneto points for condition and proper
clearance..............................................................
19. Inspect magneto for oil leakage. ..........................
20. Inspect breaker felts for proper lubrication. ..........
21. Inspect distributor block for cracks, burned
areas, corrosion, and height of contact springs....
22. Check magnetos to engine timing. .......................
23. Overhaul or replace magnetos. (See Note 11.)
24. Remove air filter and tap gently to remove dirt
particles Replace as required..............................
25. Drain carburetor and clean inlet line fuel strainer.
26. Inspect condition of carburetor heat air door and
box. (See Note 12.) .............................................
27. Inspect vent lines for evidence of fuel or oil
seepage................................................................
28. Inspect intake seals for leaks and clamps for
tightness. ..............................................................
29. Inspect all air inlet duct hoses. (Replace as per
latest revision Piper Service Bulletin No. 356.) ....
30. Inspect flexible fuel lines condition. ......................
31. Replace flexible fuel lines. (See Note 8.)
32. Inspect fuel system for leaks. ...............................
33. Clean electric fuel pump screen and check
operation. .............................................................
34. Overhaul or replace engine driven and electric
fuel pumps. (See Note 11.)
35. Remove and clean fuel filter bowl and screen
Clean at least every 90 days. ...............................
36. Inspect vacuum pump and lines...........................
37. Overhaul or replace vacuum pump. (See Note
11.)
38. Inspect throttle, carburetor heat, mixture, and
propeller governor controls for security, travel,
and operating conditions. .....................................
39. Inspect exhaust stacks, connections, and
gaskets. Replace gaskets as required. (Refer to
Maintenance Manaul, Chapter 78.) ......................
40. Inspect muffler, heat exchanger and baffles.
(Refer to latest revision of Piper Service Bulletin
879 and Maintenance Manaul, Chapter 78.) ........
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B. ENGINE GROUP.
WARNING: Ground magneto primary circuit prior to
beginning any engine work.
NOTE:
Read note 6 prior to beginning this
inspection group.
1.
2.
Remove engine cowling. Inspect for damage. .....
Clean and inspect cowling for cracks, distortion,
and loose or missing fasteners ............................
3. Drain oil sump. (See Note 7.) ..............................
4. Clean suction oil strainer at oil change. Inspect
strainer for foreign particles..................................
5. Clean pressure oil strainer or change full flow
(cartridge type) oil filter element. Check strainer
or element for foreign particles.............................
6. Inspect oil temperature sender unit for leaks and
security. ................................................................
7. Inspect oil lines and fitting for leaks, security,
chafing, dents, and cracks.
(See Note 8.) ........................................................
8. Clean and inspect oil radiator cooling fins............
9. Remove and flush oil radiator...............................
10. Fill engine with oil per lubrication chart. (Refer to
Maintenance Manaul, Chapter 12.) ......................
CAUTION:
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Use caution not to contaminate vacuum
pump with cleaning fluid. (Refer to
latest revision Lycoming Service
Instruction No. 1221.)
11. Clean engine. .......................................................
12. Inspect condition of spark plugs (clean and
adjust gap as required, adjust per
latest revision Lycoming Service Instruction no.
1042. ....................................................................
NOTE:
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Inspector
1000
5.
6.
Inspect spinner and back plate.............................
Inspect blades for nicks and cracks. ....................
Inspect for grease and oil leaks............................
Lubricate propeller. Refer to Maintenance
Manaul, Chapter 12.)............................................
Inspect spinner mounting brackets.......................
Inspect propeller mounting bolts and safety.
Check torque, if safety is broken. .........................
Inspect hub parts for cracks and corrosion. .........
Inspect complete propeller and spinner assembly
for security, chafing, cracks, deterioration, wear,
and proper installation. .........................................
Recondition propeller. (See Note 5.)
0
B. ENGINE GROUP (continued)
A. PROPELLER GROUP
1.
2.
3.
4.
0
50
DESCRIPTION
Refer to Notes 1, 2, 3, and 4 before
performing inspections.)
500
Perform all inspections or operations at each of the
inspection intervals as indicated by a circle (0)
100
NOTE:
Inspector
DESCRIPTION
100
Annual
500
Circle Type of Inspection
100
500
1000
50
50
Make:
1000
This form meets requirements of FAR Part 43 • Inspections must be performed by persons authorized by the FAA.
ARCHER II AND III
Model PA- PA-28-181
Serial No.
Registration No.
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NOTE:
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It is recommended that all airplanes be
fitted with a new muffler at or before
1000 hour period of muffler use.
41. Inspect breather tube for obstructions and
security. ................................................................
42. Inspect crankcase for cracks, leaks, and security
of seam bolts. .......................................................
43. Inspect engine mounts for cracks and loose
mountings.............................................................
44. Inspect all engine baffles......................................
45. Inspect all wiring connected to the engine or
accessories. ......................................................... 0
If fouling of spark plugs are apparent,
rotate bottom plugs to upper plugs.
13. Inspect spark plug cable leads and ceramics for
corrosion and deposits. ........................................ 0
14. Check cylinder compression. (Reference: AC
43.13-1A.).............................................................
0
Signature of Owner:
230 1039
-1-
REISSUED: JULY 30, 1994
2.
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8.
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11.
12.
13.
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15.
16.
17.
18.
19.
20.
Inspect cabin entrance, doors, and windows for
damage and operation. ........................................
Inspect window sealants for cracks and
deterioration. Reseal if necessary. ......................
Inspect upholstery for tears. .................................
Inspect seats, seat belts, security brackets, and
bolts......................................................................
Check trim operation. (See Note 15.)..................
Inspect rudder pedals...........................................
Inspect parking brake and brake handle for
operation and cylinder leaks.................................
Inspect control wheels, column, pulleys, and
cables for condition. (See Note 16.) ....................
Inspect flap control cable attachment bolt.
(Refer to latest revision of Piper Service Bulletin
965.) .....................................................................
Inspect landing, navigation, cabin, and
0
instrument lights. ..................................................
Inspect instruments, lines, and attachments. .......
Inspect gyro operated instruments and electric
turn and bank. (Overhaul or replace as
required.) ..............................................................
Replace central air filter........................................
Clean or replace vacuum regulator filter...............
Inspect altimeter. Calibrate altimeter system per
if appropriate. ..............................
FAR 91.
Check fuel selector valve operation. ....................
Inspect condition of heater controls and ducts. ....
Inspect air vents condition and operation.............
Inspect condition of air conditioning ducts............
Remove and clean air conditioning evaporator
filter.......................................................................
D. FUSELAGE AND EMPENNAGE GROUP
1.
2.
Remove inspection plates and panels..................
Inspect baggage door, latch, and hinges. ............
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3a. Archer II - Inspect battery, box, cables, and
securing straps. Inspect at least every 30 days.
Flush box as required and fill battery per box
instructions. ..........................................................
3b. Archer III - Inspect battery condition and security.
Clean and recharge acid recovery (vent) jar.
(Refer to Maintenance Manaul, Chapter 24) ........
4. Inspect electronic installation. ..............................
5. Inspect bulkheads and stringers for damage. ......
6. Inspect antenna mounts and electric wiring. ........
7. Inspect air conditioning system for Freon leaks.
(See Note 13.) ......................................................
8. Inspect Freon level in sight gauge of receiverdehydrator. (Refer to Maintenance Manaul,
Chapter 21 and see Note 13.) ..............................
9. Inspect air conditioning condenser air scoop
rigging. (See Note 23) .........................................
10. Inspect fuel lines, valves, and gauges for
damage and operation. ........................................
11. Clean screen in fuel pumps..................................
12. Remove, drain, clean fuel strainer bowl, and
screen...................................................................
13. Inspect security of all lines. ..................................
14. Inspect vertical fin and rudder surfaces for
damage. ...............................................................
15. Inspect rudder hinges, horn, and attachments for
damage and operation. ........................................
16. Inspect rudder control stops. Verify stops are not
loose an locknuts are tight....................................
17. Inspect vertical fin attachments. ...........................
18. Inspect rudder hinge bolts for excess wear.
Replace as required. ............................................
19. Inspect stabilator surfaces for damage. ...............
20. Inspect stabilator, tab hinges, horn, and
attachments for damage and operation................
21. Inspect stabilator control stops, verify stops are
not loose and locknuts are tight............................
22. Inspect stabilator attachments. (See latest Piper
Service Bulletin 856.) ...........................................
23. Inspect stabilator and tab hinge bolts and
bearings for excess wear. Replace as required. .
24. Inspect stabilator trim mechanism........................
25. Inspect aileron, rudder, stabilator primary control
cables, and stabilator trim cables, turnbuckles,
guides, and pulleys for safety, damage, and
operation. (See Note 16.) ....................................
26. Use a tensiometer to inspect all cable tensions.
(See Note 17.) ......................................................
27. Clean and lubricate stabilator trim drum screw. ...
28. Clean and lubricate all exterior needle bearings. .
29. Lubricate per lubrication chart. (Refer to
Maintenance Manaul, Chapter 12.) .....................
30. Inspect anti-collision light for security and
operation. .............................................................
31. Inspect security of autopilot bridle cable clamps.
(See Note 18.) ......................................................
32. Inspect all air ducts, electrical leads, lines, radio
antenna leads, and attaching parts for security,
routing, chafing, deterioration, wear, and
proper,installation. ................................................
33. Inspect ELT installation, battery and antenna
condition. (See the latest revision Piper Service
Letter no. 820.) .....................................................
34.Install inspection plates and panels .......................
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E. WING GROUP
0
230 1039
0
D. FUSELAGE AND EMPENNAGE GROUP
(continued)
C. CABIN GROUP
1.
1000
46. Inspect rubber engine mount bushings for
deterioration. Replace as required. .....................
47. Inspect firewall seals. ...........................................
48. Inspect alternator drive belt condition and
tension..................................................................
49. Lubricate alternator idler pulley (if installed) per
lubrication chart. ...................................................
50. Inspect condition of alternator and starter, and
related electrical connections. ..............................
51. Inspect security of alternator mounting. ...............
52. Inspect air conditioning compressor oil level.
(See Note 13.) ......................................................
53. Inspect compressor belt condition and tension.
(90 to 100 lb.) .......................................................
54. Inspect compressor clutch security and wiring.
(See Note 14.) ......................................................
55. Inspect security of compressor mounting.............
56. Check fluid in brake reservoir. Fill as required. ... 0
57. Lubricate all controls. (Refer to Maintenance
Manaul, Chapter 12.)............................................
58. Overhaul or replace propeller governor. (See
Note 11.)
59. Complete engine overhaul or replace with factory
rebuilt. (Refer to latest revision of Textron
Lycoming Service Letter 201.)
60. Install engine cowl. ............................................... 0
500
B. ENGINE GROUP (continued)
100
DESCRIPTION
50
Perform all inspections or operations at each of the
inspection intervals as indicated by a circle (0)
Inspector
Inspector
1000
100
DESCRIPTION
500
Annual
50
Circle Type of Inspection
100
500
1000
50
1.
-2-
Remove inspection plates and fairings.................
REISSUED: JULY 30, 1994
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230 1039
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Inspect float attachment fittings............................
Inspect floats for damage .....................................
Inspect pulleys and cables (see Note 16) ............
H. OPERATIONAL INSPECTION
F. LANDING GEAR GROUP
Inspect oleo struts for proper extension. Check
fluid level as required. .......................................... 0
Inspect nose gear steering control and travel. .....
Inspect wheels for alignment................................
Put airplane on jacks. ...........................................
Inspect tires for cuts, uneven or excessive wear,
and slippage. ........................................................
Remove wheels, clean, check, and repack
bearings................................................................
Inspect wheels for cracks, corrosion, and broken
bolts......................................................................
Inspect tire pressure............................................. 0
Inspect brake lining and disc for condition and
wear......................................................................
Inspect brake backing plates for condition and
wear......................................................................
Inspect brake lines. ..............................................
Inspect shimmy dampener. ..................................
Inspect gear forks for damage..............................
Insect Archer II cast main landing gear oleo
housing torque ling attach lugs for cracks.
(Refer to Maintenance Manaul, Chapter 32 and
see note 26) .........................................................
Inspect oleo struts for fluid leaks and scoring. .....
Inspect gear struts and mounting bolts for
condition and security...........................................
Inspect torque links for cracks, bolts for
condition and security. (Serial No’s. 28-7690001
thru 28-7890231 refer to latest Piper Service
Letter 842.) ...........................................................
Check torque link assembly for excessive side
play. ......................................................................
Inspect all hydraulic lines, electrical leads, and
attaching parts for security, routing, chafing,
deterioration, wear, and proper installation. .........
Lubricate per lubrication chart. (Refer to
Maintenance Manaul, Chapter 12.) ...................... 0
Remove airplane from jacks.................................
0
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G. FLOAT GROUP (Applicable to float equipped
Archer I and Archer II only)
2.
1.
500
Inspect surfaces and tips for damage, loose
rivets, and condition of walk-way..........................
3. Inspect tip light shield for cracks, bonds,
corrosion, or other damage. .................................
4. Inspect aileron hinges and attachments...............
5. Inspect aileron control stops, verify stops are not
loose and locknuts are tight..................................
6. Inspect aileron cables, pulleys, and bellcranks
for damage and operation. (See Note 16.)..........
7. Inspect flaps and attachments for damage and
operation. .............................................................
8. Inspect condition of bolts used with hinges.
Replace as required. ............................................
9. Lubricate per lubrication chart. (Refer to
Maintenance Manaul, Chapter 12.) ...................... 0
10. Inspect wing attachment bolts and brackets. .......
11. Inspect wing fore and aft attach fittings for
security, corrosion and condition. See to note
25.) .......................................................................
12. Inspect fuel tanks and lines for leaks and water.
(See Note 23.) ......................................................
13. Fuel tanks marked for capacity.............................
14. Fuel tanks marked for minimum octane rating. ....
15. Inspect fuel cell vents. (See Note 20.).................
16. Inspect all air ducts, electrical leads, lines, and
attaching parts for security, routing, chafing,
deterioration, wear, and proper installation.........
17.Install inspection plates and fairings. .....................
50
DESCRIPTION
E. WING GROUP (continued)
100
Perform all inspections or operations at each of the
inspection intervals as indicated by a circle (0)
Inspector
Inspector
1000
100
500
DESCRIPTION
Annual
50
Circle Type of Inspection
100
500
1000
50
21.
Check fuel pump and fuel tank selector ...............
Check fuel quantity, pressure and flow readings..
Check oil pressure and temperature ....................
Check alternator output ........................................
Check manifold pressure......................................
Check carburetor air. ............................................
Check parking brake. ...........................................
Check operation of auxiliary vacuum pump
system, if installed. (See note 21.) ......................
Check vacuum gauge...........................................
Check gyros for noise and roughness..................
Check cabin heater operation. .............................
Check magneto switch operation. ........................
Check magneto rpm variation. .............................
Check throttle and mixture operation. (See latest
revision Piper Service Bulletin No. 448.) ..............
Check propeller smoothness................................
Perform maximum power static rpm check per
Maintenance Manaul, Chapter 71. .......................
Check engine idle.................................................
Check electronic equipment operation. ................
Check air conditioner compressor clutch
operation. .............................................................
Check air conditioner condenser scoop
operation. .............................................................
Check operation of autopilot, including automatic
pitch trim, and manual electric
trim (if installed). (Refer to note 22.)....................
I. GENERAL
1.
2.
3.
4.
5.
Verify aircraft conforms to FAA Specifications ......
Comply with all latest revision FAA Airworthiness
Directives..............................................................
Comply with all latest revision Manufacturers
Service Bulletins and Letters................................
Check for proper flight manual .............................
Verify aircraft papers in proper order....................
— END —
-3-
REISSUED: JULY 30, 1994
NOTES
1.
2
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
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20.
21.
22.
23.
24.
25.
26.
230 1039
Refer to last card of Piper parts price list Aerofiche, for a check list of current revision dates to Piper inspection reports
and manuals.
All inspections or operations are required each inspection interval as indicated by a (O). Both the annual and 100 hour
inspections are complete aircraft inspections, identical in scope. The 500 and 1000 hour inspections are extensions of
the annual or 100 hour inspection and require more detailed aircraft examination, overhaul, or replacement of major
components. Inspections must be by FAA authorized persons.
Piper Service Bulletins are of special importance and Piper considers compliance mandatory.
Piper Service Letters are product improvements and service hints pertaining to aircraft servicing, and require careful
attention.
Recommended flight time between reconditioning of Sensenich fixed-pitch metal propellers is 1000 hours, if propeller
has no prior damage. Reconditioning is removal of fatigued surface metal and accumulated small nicks too numerous
to repair individually. Contact a Sensenich factory approved repair station. (Refer to latest revision of Sensenich
Service Letter no. 80-1.)
Power plant inspections are based on the engine manufacturer’s operator’s manual. Changes to the engine
manufacturer’s operator’s manual will supersede or supplement inspections outlined lined in this report. Refer to
latest revision of Textron Lycoming Service Letter No. 114
Intervals between oil changes can be increased as much as 100 percent on engines equipped with full flow cartridge
type oil filters, if element is replaced each 50 hours of operation. Refer to latest revision Lycoming Service Bulletin
480 for additional information.
Replace engine compartment flexible hoses (fuel, oil, etc.) every 1000 hours, 8 years or at engine TBO, whichever
comes first. Refer to latest revision of Textron Lycoming Service Bulletin 240 and latest revision of Textron Lycoming
Service Letter L201B.
Check cylinders for evidence of excessive heat (look for burned paint on cylinders. This condition indicates internal
cylinder damage and, if found, its cause must be found and corrected before aircraft returns to service.
Heavy discoloration and appearance of seepage at cylinder head and barrel attachment area is usually due to
emission of thread lubricant used during barrel assembly at the factory, or by slight gas leakage stopping after cylinder
is in service awhile. This condition is not harmful to engine performance and operation. If leakage exceeds these
condition, replace cylinder.
At every 400 hours of engine operation, remove rocker box covers and check for freedom of valve rockers when
valves are closed. Look for evidence of abnormal wear or broken parts in area of valve tips, valve keeper, springs,
and spring seat. If wear is found, remove the cylinder and all components (including piston and connecting rod
assembly) and inspect for further damage. Replace any parts not conforming to limits in latest revision for Textron
Lycoming Service Table of Limits SSPO 1776.
Replace (or overhaul, if applicable) at engine overhaul or 5 years, whichever comes first. (For engine overhaul, refer
to latest revision of Textron Lycoming Service Bulletin 240 and Service Letter L201).
Check throttle body attaching screws for tightness. Tighten screws to a torque of 40 to 50 inch-pounds.
Compressor oil level should not be checked unless a Freon leak has occurred, requiring an addition of Freon to
the system. CAUTION: Environmental regulations may require special equipment and procedures be utilized
when charging air conditioning system with Freon.
Clean any traces of oil from clutch surface.
If airplane has electric trim system refer to latest revision Piper Service Bulletin no. 556.
Examine cables for broken strands by wiping the cable with a cloth along the entire length of the cable. Visually
inspect the cable thoroughly for damage not detected by the cloth. Replace damaged or frayed cables. Refer to
Chapter 27 and the latest edition of FAA Advisory Circular 43.13-1A, Paragraph 198.
Maintain cable tensions specified in chapter 27.
Check security and condition of autopilot servo bridle cables, clamps, and sheer pin per latest revision of Piper
Service Letter No. 695.
Replace flexible fuel tank supply hose at engine overhaul.
Replace fuel tank vent line flexible connections as required, but no later than 1000 hours time-in-service.
The Airborne auxiliary vacuum pump/motor assembly (4A3-1) must be removed from service and replaced at 500
hours operating time as indicated on the elapsed time indicator, or at 10 years of installed time in the aircraft,
whichever comes first.
Refer to Flight Manual Supplement for preflight and flight check for intended function in all modes.
Pressure check all fluid hoses in fuselage and wing areas after 10 years time-in-service. Visually check for leaks.
Hoses that pass inspection may remain in service and checked thereafter each five years time-in-service.
Replace compressor belt each 1000 hours time-in-service, or 3 years, whichever comes first.
Inspect area around fore and aft attach fittings for evidence of wet interior insulation. Replace as necessary.
On Archer II airplanes used for training, and utilizing cast main gear cylinder housings, inspect the housing radii at the
torque link attach lugs for cracks after the first 2000 hours time-in-service. Thereafter, the inspection must be
performed each 100 time-in-service. Replacing the cast housings with a forged housings (Piper p/n 65490-0) will
eliminate the need for this inspection.
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REISSUED: JULY 30, 1994